Boeing 747-400 vs. Lockheed U-2
... or view the full comparison list
here.
Boeing 747-400 |
versus |
Lockheed U-2 |
70.56 m |
231 ft 10 in |
length |
19.2 m |
63 ft 0 in |
19.3 m |
63 ft 4 in |
height |
4.8 m |
15 ft 9 in |
59.49 m |
195 ft 4 in |
wingspan |
32 m |
105 ft |
Pratt & Whitney PW4000, General Electric CF6 -80C2 or Rolls-Royce RB211 -524G/H |
engines |
1 × General Electric F118-101 |
Around 60,000 to 70,000 pounds |
thrust per engine |
17,000 lbf (76 kN) |
Around 240,000 to 280,000 pounds |
total thrust |
17,000 lbf (76 kN) |
396,834 kg |
875,000 lb |
MTOW |
18,144 kg |
40,000 lb |
13,492 km |
7,285 nmi |
range |
6,090 nm |
11,278 km |
939 km/h |
584 mph |
cruise speed |
475 mph |
764 km/h |
Typically accommodates 416 passengers in a three-class layout |
capacity |
|
|
|
rotor diameter |
|
|
|
|
rate of climb |
|
|
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.